View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 56746U 26145.65250176 +.00000000 +00000-0 +71071-3 0 00000
2 56746 97.4959 0.4328 0002657 87.9228 272.2336 15.66015303 01
| Epoch (UTC): | 25 May 2026 15:39:36 |
| Eccentricity: | 0.0002657 |
| inclination: | 97.4959° |
| perigee height: | 369 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 0.4328° |
| argument of perigee: | 87.9228° |
| revolutions per day: | 15.66015303 |
| mean anomaly at epoch: | 272.2336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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